DE2027371C3 - Flugkörper mit Stabilisierungsflügeln und einem Festreibstoff-Triebwerk mit zwei gesonderten Treibsätzen - Google Patents

Flugkörper mit Stabilisierungsflügeln und einem Festreibstoff-Triebwerk mit zwei gesonderten Treibsätzen

Info

Publication number: DE2027371C3
Authority: DE; Germany
Prior art keywords: missile; nozzles; gravity; center; stabilizing wings
Prior art date: 1969-06-06
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Expired

Application number

DE2027371A

Other languages

German (de)

English (en)

Other versions

DE2027371B2 (de

DE2027371A1 (de

Inventor

Gunnar Jacobson

Olof Bertil Olsson

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Saab Bofors AB

Original Assignee

Bofors AB

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

1969-06-06

Filing date

1970-06-04

Publication date

1980-01-03

1970-06-04 Application filed by Bofors AB filed Critical Bofors AB

1970-12-10 Publication of DE2027371A1 publication Critical patent/DE2027371A1/de

1979-05-03 Publication of DE2027371B2 publication Critical patent/DE2027371B2/de

1980-01-03 Application granted granted Critical

1980-01-03 Publication of DE2027371C3 publication Critical patent/DE2027371C3/de

Status Expired legal-status Critical Current

Links

239000003380 propellant Substances 0.000 title claims description 32
230000000087 stabilizing effect Effects 0.000 title claims description 23
239000004449 solid propellant Substances 0.000 title claims description 6
230000005484 gravity Effects 0.000 claims description 24
239000000567 combustion gas Substances 0.000 claims description 11
239000000446 fuel Substances 0.000 claims description 9
230000006641 stabilisation Effects 0.000 description 5
238000011105 stabilization Methods 0.000 description 5
238000007373 indentation Methods 0.000 description 4
239000007789 gas Substances 0.000 description 3
238000010276 construction Methods 0.000 description 2
239000002360 explosive Substances 0.000 description 1
230000001771 impaired effect Effects 0.000 description 1
230000000149 penetrating effect Effects 0.000 description 1
230000002093 peripheral effect Effects 0.000 description 1

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/70—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles

Landscapes

Engineering & Computer Science (AREA)
General Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Physics & Mathematics (AREA)
Fluid Mechanics (AREA)
Mechanical Engineering (AREA)
Aviation & Aerospace Engineering (AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Toys (AREA)

DE2027371A 1969-06-06 1970-06-04 Flugkörper mit Stabilisierungsflügeln und einem Festreibstoff-Triebwerk mit zwei gesonderten Treibsätzen Expired DE2027371C3 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
SE08063/69A SE340417B (xx)	1969-06-06	1969-06-06

Publications (3)

Publication Number	Publication Date
DE2027371A1 DE2027371A1 (de)	1970-12-10
DE2027371B2 DE2027371B2 (de)	1979-05-03
DE2027371C3 true DE2027371C3 (de)	1980-01-03

Family

ID=20273043

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DE2027371A Expired DE2027371C3 (de)	1969-06-06	1970-06-04	Flugkörper mit Stabilisierungsflügeln und einem Festreibstoff-Triebwerk mit zwei gesonderten Treibsätzen

Country Status (10)

Country	Link
US (1)	US3684215A (xx)
JP (1)	JPS4810360B1 (xx)
BE (1)	BE751547A (xx)
CH (1)	CH508863A (xx)
DE (1)	DE2027371C3 (xx)
FR (1)	FR2049166B1 (xx)
GB (1)	GB1311747A (xx)
NL (1)	NL161255C (xx)
NO (1)	NO125748B (xx)
SE (1)	SE340417B (xx)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2463909B1 (fr) *	1979-08-17	1985-10-25	Thomson Brandt	Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2500149B1 (fr) *	1981-02-17	1985-12-06	Poudres & Explosifs Ste Nale	Chargement propulsif biregime a canal en trompette comportant une section en etoile
GB2172383B (en) *	1981-06-04	1987-08-12	Aerospatiale	Guided missile system
FR2578665B1 (fr) *	1981-06-04	1988-02-12	Aerospatiale	Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede
FR2863665B1 (fr) *	1988-10-12	2007-03-30	Aerospatiale	Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur
IL101730A (en) *	1992-04-30	1995-12-31	Israel State	Moving body such as missile having wings erectable upon acceleration
US8350200B1 (en) *	2009-03-26	2013-01-08	Lockheed Martin Corporation	Passive aerosurface adjustment for static margin management
CN108562195B (zh) *	2018-01-12	2019-05-24	北京航空航天大学	一种便于调整的模块化配重装置及火箭

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB594516A (en) *	1940-09-04	1947-11-13	Charles Dennistoun Burney	Improvements in or relating to projectiles operating with rocket propulsion
US2503271A (en) *	1945-02-06	1950-04-11	Clarence N Hickman	Rocket projectile
US2816721A (en) *	1953-09-15	1957-12-17	Taylor Richard John	Rocket powered aerial vehicle
US3013494A (en) *	1957-08-09	1961-12-19	Chanut Pierre Louis Jean	Guided missile
US3127838A (en) *	1960-10-12	1964-04-07	Bombrini Parodi Delfino Spa	Retractable blade tail unit for projectiles

1969
- 1969-06-06 SE SE08063/69A patent/SE340417B/xx unknown
1970
- 1970-05-28 US US41373A patent/US3684215A/en not_active Expired - Lifetime
- 1970-06-02 NL NL7007998.A patent/NL161255C/xx not_active IP Right Cessation
- 1970-06-03 CH CH832570A patent/CH508863A/de not_active IP Right Cessation
- 1970-06-03 NO NO2161/70A patent/NO125748B/no unknown
- 1970-06-04 JP JP45048661A patent/JPS4810360B1/ja active Pending
- 1970-06-04 DE DE2027371A patent/DE2027371C3/de not_active Expired
- 1970-06-05 BE BE751547D patent/BE751547A/xx unknown
- 1970-06-05 FR FR7020862A patent/FR2049166B1/fr not_active Expired
- 1970-06-05 GB GB2737770A patent/GB1311747A/en not_active Expired

Also Published As

Publication number	Publication date
FR2049166B1 (xx)	1974-05-24
NL161255B (nl)	1979-08-15
GB1311747A (en)	1973-03-28
US3684215A (en)	1972-08-15
CH508863A (de)	1971-06-15
NO125748B (xx)	1972-10-23
DE2027371B2 (de)	1979-05-03
NL7007998A (xx)	1970-12-08
SE340417B (xx)	1971-11-15
BE751547A (fr)	1970-11-16
JPS4810360B1 (xx)	1973-04-02
NL161255C (nl)	1980-01-15
DE2027371A1 (de)	1970-12-10
FR2049166A1 (xx)	1971-03-26

Legal Events

Date	Code	Title	Description
1980-01-03	C3	Grant after two publication steps (3rd publication)
1987-06-11	8339	Ceased/non-payment of the annual fee

Publication	Publication Date	Title
DE2323244B2 (de)	1978-08-17	Flügelstabilisiertes Unterkalibergeschoß
DE2757141C2 (de)	1986-06-26	Bremsvorrichtung für einen im Flug rotierenden Körper insbes. einen Abwurfkörper
DE1954540C3 (de)	1973-09-27	Rakete mit Abschußeinrichtung
DE2936554T1 (de)	1980-12-11	An arrangement for launching interference material
DE2027371C3 (de)	1980-01-03	Flugkörper mit Stabilisierungsflügeln und einem Festreibstoff-Triebwerk mit zwei gesonderten Treibsätzen
DE2845414A1 (de)	1979-04-26	Beim ueberfliegen des ziels wirksam werdendes geschoss
DE69713760T2 (de)	2002-12-05	Geshoss von kleinem kaliber
EP0209761A1 (de)	1987-01-28	Flugkörper mit ausschwenkbaren Gleitflügeln
DE2805496C2 (de)	1987-04-16	Geschoß mit Leitflügeln
DE4321806C2 (de)	1995-06-01	Raketenmotor für eine Anlockvorrichtung
DE3715085A1 (de)	1996-05-02	Flugkörper-Spitzenverkleidungsaufbau
DE1578117A1 (de)	1971-04-15	Geschoss mit Ringleitwerk
DE2160324C2 (de)	1982-04-08	Flugkörper mit entfaltbaren Stabilisierungsflächen
EP0237711B1 (de)	1992-06-10	Treibladungsanzünder
DE1905294C3 (xx)	1976-09-02
DE3643291A1 (de)	1988-06-23	Drallstabilisiertes traegergeschoss
DE2030722C3 (de)	1981-11-05	Leuchtspureinrichtung
DE1958355A1 (de)	1970-05-27	Flugkoerpersystem
DE2726551C2 (xx)	1988-08-18
DE3804930A1 (de)	1989-08-31	Flugkoerper
DE2028539C3 (de)	1979-04-05	Raketenmotor fur Festbrennstoffe
DE2335126A1 (de)	1974-02-14	Ablenkvorrichtung fuer raketengetriebene geschosse
DE19806066B4 (de)	2004-07-08	Flugkörper gegen Reaktivpanzerung
DE68911191T2 (de)	1994-05-19	Stabilisierungsvorrichtung für Geschosse von gezogenen Läufen.
DE2159941C3 (de)	1980-07-17	Elektrische Kontakteinrichtung für eine Rakete